Attenuation in a Shock Tube due to Unsteady-Boundary-Layer Action. Mirels, H. Technical Report 1333, National Advisory Committee for Aeronautics, 1957. bibtex @techreport{mirels1957,
title = {Attenuation in a {Shock} {Tube} due to {Unsteady}-{Boundary}-{Layer} {Action}},
number = {1333},
institution = {National Advisory Committee for Aeronautics},
author = {Mirels, Harold},
year = {1957},
}
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